CN102498038B - 飞行器发动机的悬挂支柱，包括所述支柱的组件及相关联的飞行器 - Google Patents

飞行器发动机的悬挂支柱，包括所述支柱的组件及相关联的飞行器 Download PDF

Info

Publication number
CN102498038B
CN102498038B CN201080041622.9A CN201080041622A CN102498038B CN 102498038 B CN102498038 B CN 102498038B CN 201080041622 A CN201080041622 A CN 201080041622A CN 102498038 B CN102498038 B CN 102498038B
Authority
CN
China
Prior art keywords
flange
driving engine
attached
aircraft
alar part
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201080041622.9A
Other languages
English (en)
Chinese (zh)
Other versions
CN102498038A (zh
Inventor
弗雷德里克·茹尔纳德
劳伦特·拉丰
劳伦特·阿戈斯蒂尼
埃里克·雷诺
德尔菲娜·贾尔伯特
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
Airbus Operations SAS
Original Assignee
Airbus Operations GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of CN102498038A publication Critical patent/CN102498038A/zh
Application granted granted Critical
Publication of CN102498038B publication Critical patent/CN102498038B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Plates (AREA)
CN201080041622.9A 2009-09-22 2010-09-20 飞行器发动机的悬挂支柱，包括所述支柱的组件及相关联的飞行器 Expired - Fee Related CN102498038B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0956528 2009-09-22
FR0956528A FR2950323B1 (fr) 2009-09-22 2009-09-22 Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe
PCT/FR2010/051949 WO2011036385A1 (fr) 2009-09-22 2010-09-20 Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe

Publications (2)

Publication Number Publication Date
CN102498038A CN102498038A (zh) 2012-06-13
CN102498038B true CN102498038B (zh) 2014-11-12

Family

ID=42123013

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201080041622.9A Expired - Fee Related CN102498038B (zh) 2009-09-22 2010-09-20 飞行器发动机的悬挂支柱，包括所述支柱的组件及相关联的飞行器

Country Status (5)

Country Link
US (1) US8640987B2 (fr)
EP (1) EP2480455B1 (fr)
CN (1) CN102498038B (fr)
FR (1) FR2950323B1 (fr)
WO (1) WO2011036385A1 (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2950860B1 (fr) * 2009-10-01 2011-12-09 Airbus Operations Sas Dispositif d'accrochage d'un moteur a un mat d'aeronef
FR2976914B1 (fr) * 2011-06-23 2014-12-26 Snecma Structure d'accrochage d'une turbomachine
FR2978730B1 (fr) * 2011-08-03 2013-09-27 Airbus Operations Sas Berceau d'articulation de capots de soufflante supportes par ces capots en position fermee
US9211955B1 (en) 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
EP2943670B1 (fr) * 2013-01-10 2020-01-22 United Technologies Corporation Générateur de gaz double corps avec anneau de montage
GB201306674D0 (en) * 2013-04-12 2013-05-29 Rolls Royce Plc Rigid Raft for a Gas Turbine Engine
US10266273B2 (en) 2013-07-26 2019-04-23 Mra Systems, Llc Aircraft engine pylon
FR3010700B1 (fr) * 2013-09-18 2017-11-03 Snecma Dispositif de suspension d'un carter, turbomachine et ensemble propulsif
WO2015047539A1 (fr) * 2013-09-27 2015-04-02 United Technologies Corporation Systèmes de montage pour moteurs à turbine à gaz
FR3016344B1 (fr) 2014-01-10 2017-09-01 Snecma Structure de suspension d'un turbopropulseur a double helices non carenees sur un element structurel d'un aeronef a fixation rigide de la structure d'entree d'air
FR3020343B1 (fr) 2014-04-23 2017-10-27 Airbus Operations Sas Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage constituee par trois elements independants
FR3025782B1 (fr) 2014-09-16 2016-09-30 Snecma Procede et dispositif de montage d'un moteur sur un pylone d'aeronef
US10197213B2 (en) * 2017-01-26 2019-02-05 General Electric Company Systems and methods for mounting a rotatable machine
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1993266A (zh) * 2004-08-05 2007-07-04 法国空中巴士公司 用于飞行器的喷气式涡轮发动机的悬挂杆
CN1993267A (zh) * 2004-08-05 2007-07-04 法国空中巴士公司 用于飞行器的发动机组件
FR2913664A1 (fr) * 2007-03-16 2008-09-19 Aircelle Sa Nacelle pour turboreacteur double flux
FR2928347A1 (fr) * 2008-03-07 2009-09-11 Aircelle Sa Structure d'accrochage pour turboreacteur

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2303884B (en) * 1995-04-13 1999-07-14 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
US6983912B2 (en) * 2002-04-30 2006-01-10 The Boeing Company Hybrid exhaust heat shield for pylon mounted gas turbine engines
FR2862612B1 (fr) * 2003-11-25 2006-02-17 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
FR2862611B1 (fr) * 2003-11-25 2007-03-09 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
FR2873088B1 (fr) 2004-07-16 2008-04-04 France Design Sa Structure de base de vehicule a plusieurs toits rapportes et vehicules correspondants
FR2887521B1 (fr) * 2005-06-28 2007-08-17 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
FR2891246B1 (fr) * 2005-09-26 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
FR2891254B1 (fr) * 2005-09-29 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef
FR2900907B1 (fr) * 2006-05-09 2008-12-19 Airbus France Sas Ensemble moteur pour aeronef a nacelle et mat integres
FR2903076B1 (fr) 2006-06-30 2009-05-29 Aircelle Sa Nacelle structurante
FR2903666B1 (fr) * 2006-07-11 2008-10-10 Airbus France Sas Ensemble moteur pour aeronef comprenant un capotage aerodynamique de jonction monte sur deux elements distincts
FR2905990A1 (fr) 2006-09-20 2008-03-21 Snecma Sa Systeme propulsif a pylone integre pour avion.
FR2907098B1 (fr) 2006-10-11 2010-04-16 Aircelle Sa Nacelle pour turboreacteur double flux
FR2913665B1 (fr) * 2007-03-16 2009-06-05 Airbus France Sa Carenage aerodynamique arriere inferieur pour dispositif d'accrochage d'un moteur d'aeronef
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
FR2928180B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur.
FR2948636B1 (fr) * 2009-07-31 2012-01-13 Airbus Operations Sas Ensemble moteur pour aeronef dont le mat d'accrochage comprend une enveloppe structurale formant delimitation radiale interne du flux secondaire

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1993266A (zh) * 2004-08-05 2007-07-04 法国空中巴士公司 用于飞行器的喷气式涡轮发动机的悬挂杆
CN1993267A (zh) * 2004-08-05 2007-07-04 法国空中巴士公司 用于飞行器的发动机组件
FR2913664A1 (fr) * 2007-03-16 2008-09-19 Aircelle Sa Nacelle pour turboreacteur double flux
FR2928347A1 (fr) * 2008-03-07 2009-09-11 Aircelle Sa Structure d'accrochage pour turboreacteur

Also Published As

Publication number Publication date
US8640987B2 (en) 2014-02-04
US20120175462A1 (en) 2012-07-12
FR2950323A1 (fr) 2011-03-25
FR2950323B1 (fr) 2011-11-04
EP2480455A1 (fr) 2012-08-01
CN102498038A (zh) 2012-06-13
EP2480455B1 (fr) 2014-04-30
WO2011036385A1 (fr) 2011-03-31

Similar Documents

Publication Publication Date Title
CN102498038B (zh) 飞行器发动机的悬挂支柱，包括所述支柱的组件及相关联的飞行器
CN102712369B (zh) 包括发动机的悬挂元件的飞行器组件与相关联的飞行器
CN101272954B (zh) 具有单体框架的挂架
RU2354587C2 (ru) Турбореактивный двигатель для крепления на хвостовой части фюзеляжа летательного аппарата в верхнем положении
RU2383473C2 (ru) Узел двигателя для летательного аппарата
JP5642379B2 (ja) 航空機のエンジンマウント、航空機
US8613404B2 (en) Take-up device for thrust forces with connecting rods for aircraft engine attachment pylon, integrating three aligned ball joints
US8794568B2 (en) Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pins
JP5666317B2 (ja) ターボジェットエンジンの中央ケーシングを包囲する環状荷重伝達構造体を備える航空機エンジンアセンブリ
EP2027012B1 (fr) Structure de queue pour aeronef ou astronef
CN101774430A (zh) 用于安装飞行器发动机的整体结构
JP2011513112A (ja) ファンフレームから下方にずらしたエンジンの結合具を備える航空機エンジンアセンブリ
CN105000187B (zh) 用于飞行器的组件和飞行器
CN101432189A (zh) 飞机机身结构及其制造方法
JP2008509041A (ja) 航空機用ジェットエンジンパイロン
CN102695876B (zh) 机舱外壳结构、锁定式迷宫密封和风力涡轮机
CN101522524A (zh) 旁路涡轮喷气发动机的发动机舱
US20140227100A1 (en) Rotating Machine Blade with Reinforced Modular Structure
JP2008509318A (ja) 航空機用エンジンユニット
CN102310947A (zh) 制造用于飞行器发动机安装挂架的气动整流罩的肋的方法
US11465765B2 (en) Engine pylon for coupling a jet engine to a wing of an aircraft
CN103129739A (zh) 飞行器的发动机的悬挂支柱的后部空气动力整流罩
JP2009502642A5 (fr)
EP1780125B1 (fr) Système de soutien pour unité de puissance auxiliaire
US20110309189A1 (en) Rigid aircraft pylon fitted with a rib extension for taking up the moment in the lengthways direction

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20141112

Termination date: 20200920